Distributing irritant powder

ABSTRACT

The present embodiments provide apparatuses for use in launching an inhibiting powder. These embodiments comprise a source of impulse pressure that induces a propellant pressure, a barrel cooperated with the source of impulse pressure to receive the propellant pressure, inhibiting powder positioned within an interior of the barrel, a burst diaphragm secured between the source of the impulse pressure and the inhibiting powder, and an actuator that activates the source of impulse pressure to deliver an expanding gas producing an increasing pressure that is applied to the burst diaphragm where the burst diaphragm bursts when the applied pressure exceeding a burst threshold, resulting in a release of the propellant pressure into the barrel to drive the inhibiting powder from the barrel in substantially an aerosol form generating a cloud of inhibiting powder.

PRIORITY CLAIM

This application claims the benefit of U.S. Provisional Application No.60/973,447, filed Sep. 18, 2007, entitled NON-LETHAL IRRITANT POWDERCLOUD LOADS FOR PERSONAL DEFENSE LAUNCHERS, which is incorporated hereinby reference in its entirety; and this application is a continuation ofInternational Application No. PCT/U.S.08/76739, filed Sep. 17, 2008,entitled SYSTEMS, METHODS AND APPARATUS FOR USE IN DISTRIBUTING IRRITANTPOWDER, which claims the benefit of U.S. Provisional Application No.60/973,447, filed Sep. 18, 2007, entitled NON-LETHAL IRRITANT POWDERCLOUD LOADS FOR PERSONAL DEFENSE LAUNCHERS, where InternationalApplication No. PCT/U.S.08/76739 is also incorporated herein byreference in its entirety

FIELD OF THE INVENTION

The present invention relates generally to irritant powders, and moreparticularly to methods and systems of dispersing irritant powders.

BACKGROUND

For several decades, Law Enforcement agencies have used variousnon-lethal weapons to gain control of suspects, quell riots, savehostages, and the like. Many of these non-lethal weapons typicallyrequire a large launcher platform such as a shotgun, rifle or pistol todeploy projectiles. These generally large platforms can make the use ofthese launchers cumbersome in some circumstances.

To date, other than pepper spray, the general public typically has nothad access to a simple, low cost, non-lethal projectile launcher.Further, there are generally no non-lethal projectile launchers that areeasily carried and used for personal defense at home, in the car or whenon foot.

SUMMARY OF THE EMBODIMENTS

The present invention advantageously addresses the needs above as wellas other needs through the provision of the method, apparatus, andsystem for use in launching loose powder to generate a powdered cloud.Some embodiments provide apparatuses for use in launching an inhibitingpowder. These embodiments comprise a source of impulse pressure thatinduces a propellant pressure; a barrel cooperated with the source ofimpulse pressure to receive the propellant pressure; inhibiting powderpositioned within an interior of the barrel; a burst diaphragm securedbetween the source of the impulse pressure and the inhibiting powder;and an actuator that activates the source of impulse pressure to deliveran expanding gas producing an increasing pressure that is applied to theburst diaphragm where the burst diaphragm bursts when the appliedincreasing pressure exceeding a burst threshold of the burst diaphragm,where the bursting of the burst diaphragm results in a release of thepropellant pressure into the barrel to drive the inhibiting powder fromthe barrel in substantially an aerosol form generating a cloud ofinhibiting powder extending from an exit end of the barrel and out adistance from the exit end of the barrel.

Other embodiments provide launch systems. At least some of these launchsystems comprise a frame; a source of impulse pressure cooperated withthe frame; a barrel secured relative to the frame and cooperated withthe source of impulse pressure to receive a propellant pressure from thesource of impulse pressure; powder load positioned within an interior ofthe barrel, the powder load comprising a powdered inhibiting substance;a burst diaphragm secured between the source of the impulse pressure andthe powder load, wherein the burst diaphragm retains the impulsepressure from the source of impulse pressure until a pressure of aboutequal to a burst threshold of the burst diaphragm such that the burstdiaphragm bursts releasing a propellant pressure into the barrel todrive the powder load from the barrel in substantially an aerosol formgenerating a powder cloud of powder load extending from a exit end ofthe barrel.

Some embodiments provide methods of providing an individual withprotection. These methods activate, in response to an actuation, asource of impulse pressure; launch loose powder from a launch system;and generate a powder cloud comprising the loose powder that hasdimensions larger than a human torso.

A better understanding of the features and advantages of the presentinvention will be obtained by reference to the following detaileddescription of the invention and accompanying drawings which set forthan illustrative embodiment in which the principles of the invention areutilized.

BRIEF DESCRIPTION OF THE DRAWINGS

The above and other aspects, features and advantages of the presentinvention will be more apparent from the following more particulardescription thereof, presented in conjunction with the followingdrawings wherein:

FIG. 1 depicts a simplified cross-sectional diagram of a launch systemaccording to some embodiments;

FIG. 2 shows a simplified cross-sectional view of a launch system,similar to that of FIG. 1, with a membrane powder load comprising powderretained within a membrane;

FIG. 3 depicts a simplified cross-sectional view of the launch system,similar to the launch systems of FIGS. 1-2, with a powder load,according to some embodiments, comprising the membrane powder load,comprising powder retained within a membrane, and a projectile;

FIG. 4 depicts a simplified cross-sectional view of the launch system,similar to the launch systems of FIGS. 1-2, with a powder load,according to some embodiments, comprising powder and a projectile;

FIG. 5 depicts a simplified cross-sectional view of the launch system,similar to the launch systems of FIGS. 1-2, with a powder load,according to some embodiments, comprising powder and a projectile with adivider or separator positioned between the powder and the projectile;

FIG. 6 depicts a simplified cross-sectional view of a launch systemaccording to some embodiments;

FIG. 7 depicts a simplified cross-sectional view of the frame of thelaunch system of FIG. 6;

FIG. 8 depicts a simplified cross-sectional view of the barrel assemblyof the launch system of FIG. 6, according to some embodiments;

FIG. 9 depicts an enlarged view of a portion of the barrel assembly ofFIG. 8;

FIG. 10 show a simplified front view of a driver that can be employedwithin the launch system depicted in FIGS. 6-7;

FIG. 11 show a simplified side view of the driver of FIG. 10 that can beemployed within the launch system depicted in FIGS. 6-7;

FIG. 12 depicts a simplified block diagram representation of a powdercloud generated following the activation of a launch system directed ata target;

FIGS. 13-14 depict a side view and a cross-sectional view, respectively,of a launch system according to some embodiments

FIG. 15 depicts a side view of a frame of the launch system depicted inFIGS. 13-14;

FIG. 16 depicts a simplified flow diagram of a process of assembling alaunch system, such as the launch systems depicted in or more of FIGS.6-9 and 13-15; and

FIG. 17 depicts a simplified flow diagram of a process of activating alaunch system, such as one of launch systems depicted in FIGS. 6-9 and13-15.

Corresponding reference characters indicate corresponding componentsthroughout the several views of the drawings. Skilled artisans willappreciate that elements in the figures are illustrated for simplicityand clarity and have not necessarily been drawn to scale. For example,the dimensions of some of the elements in the figures may be exaggeratedrelative to other elements to help to improve understanding of variousembodiments of the present invention. Also, common but well-understoodelements that are useful or necessary in a commercially feasibleembodiment are often not depicted in order to facilitate a lessobstructed view of these various embodiments of the present invention.

DETAILED DESCRIPTION

The present embodiments provide a launching system or device that whenactivated expels a cloud of irritant powder towards a target, such as athreatening target, as a means of non-lethal defense and/or for subduinga target. This irritant cloud may have a distracting, incapacitatingand/or repelling effect on the target, be it a human or animal. Theirritant and distraction effects on the target may allow the user toretreat to a safer location, get away from an attacker, or if used bylaw enforcement or security personnel, subdue an individual for captureand/or arrest. The concept of a small handheld powder launch system canhave many embodiments depending on the desired application. The basicoperation, however, is typically similar. When threatened by an attackeror animal, for example, a user generally points or aims the launchsystem in the threat direction and activates the system, for examplethrough a triggering mechanism, that results in the substantiallyinstantaneous deployment of an irritant powder payload cloud and/or anon-lethal projectile towards the target.

There are many advantages to a device that deploys a simple blast ofirritant cloud from the muzzle of a compact self defense launchingsystem. In some embodiments, an irritant powder is launched towards thetarget(s) that generates a cloud comprised at least partially of theirritant powder with the intention that the cloud contacts the target(s)directly, drifting on air currents towards the target(s), or justplacing a barrier irritant cloud between the user and the threat.

Therefore, the launching of a non-lethal powder, to generate a powderirritant cloud, launched from a compact system provides many advantagesover conventional projectiles and/or other self defense devices. Forexample, a powder irritant cloud does not require a precise aim point onthe target to affect the target such as with a projectile. Further,unlike most conventional projectiles, the powder irritant cloud canaffect more than one threatening targets due to its relatively largevolume and ability to float on the air currents. A powder irritant cloudcan utilize a cross or back wind to further disperse its irritanttowards distant target(s). Unlike solid projectiles, a powder irritantcloud can hang in the air and be an effective temporary barrier betweenthe user and the threat, and unlike pepper spray the powder cloudtypically is visible. Still further, devices that launch someprojectiles, in some areas of the United States and the World, may beconsidered a weapon, e.g., launching a projectile carrying an inhibitingsubstances (such as some projectiles described in U.S. Pat. Nos.7,194,960; 6,546,874; 6,393,992; and 5,965,839, and Patent ApplicationPublication Nos. 2005/0188886 and 2006/0027223, all of which areincorporated herein by reference in their entirety) may be considered,in some areas of the United States or the World, a chemical weapon,while the launching of a loose powder that rapidly deploys into a cloudof inhibiting powder is not considered a weapon and can be carriedand/or used by the general public and/or non-law enforcementindividuals. Many other advantages are provided by a launch system thatlaunches loose powder to generate a cloud of irritant powder asdescribed below and will be apparent to those skilled in the art.

The powder launch systems of the present embodiments can utilize anynumber of different types of impulse energy sources to eject and/orotherwise launch the loose powder, including impulse sources employedwithin compact hand held devices. One or more of these different typesof impulse energy sources are used in launch systems to propel thenon-lethal powder loads of the present embodiments toward a target. Forexample, the impulse energy source can be from a launch system using thepressure impulse from a conventional firearm primer; an electricallyfired primer; a burning gas generator common to automobile airbagtechnology; known gunpowder technology; by spark ignition of propane,butane or other hydrocarbons; sources of compressed gas such canisters,cylinders or cartridges of compressed gas (e.g., such as found inrefillable paintball gas cylinders); replaceable compressed gascartridges (e.g., cartridges such as used in air pistols and inflationdevices); and other such sources of impulse pressure and/or combinationsof sources of impulse pressure. For example, by utilizing disposableand/or replaceable compressed gas cartridges filled with air, nitrogen,carbon dioxide and/or other gases, some launch systems of the presentembodiments may be fabricated as a disposable (e.g., one time use)launch system, and/or a portion of the launch system can be disposableand replaced in an easily reloadable launch system.

As described above, the launch systems according to some embodimentslaunch a loose powder that rapidly generates a cloud of powder extendingfrom the launch system. Launch systems and/or method of someimplementations can launch one load or multiple loads at a time or insuccession. A launch system may be capable of one or multiple launchingsthrough one or multiple barrels using various configurations. The launchsystems of some embodiments provide a source of gas impulse in abarreled device. The choice of impulse gas energy can depend on manyfactors, such as but not limited to, desired design, launch system sizeand/or weight, desired powder cloud dispersion, size and/or weight of alaunch load, and/or other application factors. As introduced above, thepowder loads of the present embodiments can be utilized with manyexisting launchers, and/or launch systems utilizing impulse pressuremechanisms (e.g., impulse gas) designed specifically to launch irritant,non-lethal powder loads described herein.

FIG. 1 depicts a simplified cross-sectional diagram of a launch system100 according to some embodiments. The launching system includes a frameor body 110 and a barrel assembly 112. Within the frame 110 is mounted asource of impulse pressure 114. The barrel assembly 112 includes anentry orifice or opening 116, a barrel or barrel bore 118 with an exitend 120 opposite from the entry opening 116. In some implementations,the frame 110 is removably mounted with the barrel assembly 112 suchthat the entry opening 116 is cooperated with the source of impulsepressure 114 allowing the impulse pressure to enter the barrel 118, uponactivation of an actuator (not shown), providing a propellant pressureinto the barrel 118. The removable mounting can include threading 122,spring loaded pins, pin and grooves and substantially any other suchmethods or combination of methods of securing that, at leasttemporarily, fixes the frame 110 with the barrel assembly 112 while thesource of impulse pressure 114 generates and directs the impulsepressure into the barrel 118.

A powder load 124 comprising powder that is unenclosed and is positionedwithin the barrel 118. The powder load 124 is a loose powder load inthat at least a majority of the powder 124 upon being ejected from thebarrel 118 is loose and unenclosed to rapidly disperse into the powdercloud extending from substantially the exit end 120 of the barrel 118 asdescribed above and further below. The powder load 124 is propelled,upon activation of the launch system 100, along the barrel 118 by thepropulsion pressure and launched or ejected from the exit end 120 of thebarrel assembly 112. In some implementations, a pusher or plunger 126 ispositioned with the barrel 118 adjacent the powder load 124, between thesource of impulse pressure 114 and the powder load 124 such that thepropulsion force is directed against the pusher 126 to drive the pusheralong the barrel 118, which in turn pushes the powder load 124 along andout of the barrel assembly 112. Typically, the pusher 126 is configuredto establish a seal with the interior surface of the barrel 118 so thatsubstantially all, and preferably all of the propulsion pressure doesnot leak around the pusher 126 and is thus substantially maintainedbehind the pusher 126. Further in some instances, the pusher 126 can beconfigured to provide equal distribution of the propulsion pressureand/or focus the propulsion pressure, for example, by including arounded or tapered inlet, not shown, in the surface of the pushing thatreceives the propulsion pressure. In other embodiments, however, thepusher 126 is not included and the source of impulse pressure 114directs the propulsion pressure directly on the powder load 124.

The pusher 126 can be configured from substantially any relevantmaterial that can receive the propulsion pressure and travel along thebarrel 118 to drive the powder load 124 from the barrel assembly 112 ata desired velocity. Further, it is desirable that the pusher 124 berelatively light weight so that it is rapidly decelerates upon leavingthe barrel assembly 112 to fall to the ground, typically before reachinga target. Additionally and/or alternatively, the pushing can beconfigured to have a relatively large wind drag to aid in deceleratingthe pusher upon exiting the barrel assembly 112. The pusher 126 can befabricated from any number of materials such as, but not limited to,urethane foam, polymer foam, Styrofoam, paper, cardboard, plastic,rubber, and/or other such similar materials or combinations ofmaterials.

A seal or retaining member 128 can further be incorporated into thebarrel 118 in some implementations to retain the powder load 124 withinthe barrel 118 and/or seal the powder load 124 within the barrelproviding a barrier between the powder load and exterior environmentalconditions. Typically, the seal 128 establishes a seal and/or is securedwithin the barrel 118 to establish a seal with the interior surface ofthe barrel 118 to protect the powder load 124 from the environment. Theseal 128 is shown in FIG. 1 being positioned within the barrel 118;however, the seal can extend from the exterior of the barrel into thebarrel. Additionally or alternatively, a cap or other structure (notshown) can be positioned on the exit end 120 of the barrel 118 and/orcan extend into the barrel to provide, in part, an additional seal tokeep foreign objects out of the barrel 118 and/or to provide anindication that the launch system 100 has not been activated and thatthe barrel assembly 112 contains a powder load 124 to be launched. Stillother structures can be incorporated with the exit end 120 of the barrel112 in those instances where a cap is not included to provide anindication of whether the barrel assembly 112 has been previouslyactivated to launch the powder load.

The seal 128 (and/or cap when present) is also typically constructed torapidly decelerate upon being driven from the barrel assembly 112, andcan be fabricated from any number of materials such as, but not limitedto, paper, cardboard, urethane foam, polymer foam, Styrofoam, plastic,rubber, wax, paraffin and/or other such similar materials orcombinations of materials. In some implementations the seal 128 isfurther secured, such as glued to the interior surface of the barrel 118to enhance and/or ensure the seal and to retain the powder load 124. Theglue can be selected to readily break upon a sufficient pressure beingapplied by the propulsion pressure allowing the seal 128 to detach fromthe interior surface of the barrel 118 and be ejected from the barrelassembly 112. The glue can be substantially any relevant glue, and insome instances is waterproof or water resistant glue, such as but notlimited to TiteBond III™ or other relevant waterproof and/or waterresistant glues. Similarly, a retaining member, such as an O-ring, maybe employed to maintain the positioning of the seal 128 (and/or pusher126) within the barrel 118. Additionally or alternatively, the seal 128can be constructed of a material, or be assembled with weakeningfeatures that allow the seal to at least partially break apart when thepropulsion pressure drives the powder load 124 against the sealreleasing the powdered load to be driven along and out of the barrelassembly 112.

The powder load 124 comprises a powder that is propelled along thebarrel and ejected from the exit end 120 of the barrel assembly 112 insubstantially an aerosol to generate a powdered cloud extending from theexit end 120 of the barrel toward a target, and in some instances abouta target when the target is within range. The powder load 124, in someembodiments as depicted in FIG. 1, is free and loose and retained by thepusher 126, the seal 128 and the interior surface of the barrel 118 suchthat the powder load 124 is in contact with the interior surface of thebarrel 118 prior to and while being driven along the barrel assembly 112to be ejected from the exit end 120 of the barrel 118. Typically, whenthe barrel 118 is loaded with the pusher 126, and loose powder 124, theloose powder is in an uncompressed state, and in some instances is notpacked or compressed when added to the barrel 118. In other embodiments,however, the loose powder may be partially tapped or compressed, may beinserted as a tablet, may be retained in a membrane or film prior toactivation of the launch system 100, and/or other such configurationsthat are ejected from the barrel assembly 112 as loose powder insubstantially a loose, free and in some instances an aerosol state.

The powder load 124, as described above, typically includes one or morepowdered irritant and/or inhibiting substances. The irritating and/orinhibiting powder can comprise one or more irritants such as, but notlimited to: one or more capsaicinoids; capsaicin; nonivamide; PAVA;oleoresin capsaicinoid (OC); a pepper derived irritant; powdered teargas (CS or CN); and/or maloderants. The powder irritants may benaturally occurring or synthetically produced. In some implementations,the powder load 124 may be pure irritant powder or may be mixed with oneor more types of inert powders to achieve a desired concentration ofirritant effect on a target. Inert powders such as barium sulfate, babypowder, cornstarch, talc, trisodium phosphate, silicon dioxide, flour,baking powder, chalk, gypsum and/or similar non-toxic inert powders maybe used to achieve the desired irritant concentration and give morevisibility to the cloud. Relatively “heavy mass powders” such as bariumsulfate or other similar non-toxic heavy powders may be added to thepowder mixture to achieve a further launching or throw distance for thepowder cloud in some implementations. Visually colored, ultraviolet (UV)fluorescent and/or other such marking powders may additionally oralternatively be also be used or added to the mixture to achieve amarking function if desired. Inert powder or inert powder mixture loadscan also be used without adding the irritant powder for the purpose of atraining or demonstration load that simulates the cloud performance ofthe irritant powder loads. The powder load 124 can comprise powder, insome implementations, as described in related U.S. Pat. Nos. 7,194,960;6,546,874; 6,393,992; and 5,965,839, and Patent Application PublicationNos. 2005/0188886; and 2006/0027223, all of which are incorporatedherein by reference in their entirety.

As described above, the powder load 124 is ejected from the exit end 120of the barrel assembly 112 to generate the cloud of inhibiting powder.To achieve the desired cloud in some instances the powdered load 124 isexpelled from the barrel assembly 112 as an aerosol that rapidly expandsas it travels away from the barrel assembly 112 and launch system 100.The powder load configuration and/or particle sizes of the powder loadcan affect the aerosolizing effect. In some embodiments, an averageparticle size of at least the inhibiting powder portion of the powderload 124 is less than about 200 microns, and typically is less thanabout 100 microns, for example, the particle sizes can be between 5-100microns, where smaller irritant powder particles typically aids in thehang time or time of suspension of the irritant powder particles andthus the cloud. Other components of the powder load may have largerparticle sizes. For example, weighting particles may have larger sizes,where the weighting particles aid in dispersing the launched inhibitingpowder.

The aerosolizing effect is also, at least in part, dependent on theamount of propulsion force applied and/or the speed at which the loosepowder is propelled from the barrel assembly 112. In someimplementations the propulsion force applied to the powder load 124 isgreater than 200 psi, and typically greater than 400 psi. The amount ofpropulsion force is further dependent on the size and/or weight of thepowder load 124 (and pusher 126 and seal 128 when relevant). Forexample, with a powder load 124 having a weight of about 5 grams, apropulsion force of over 700 psi can effectively launch the powder load,in some implementations, to generate an expanding cloud that is greaterthan about 8 feet deep extending from a position of the exit end 120 atthe time of launch, and with a width (generally perpendicular to thedepth at about 8 feet) of at least about 3 feet. Various cloud sizes,shapes and depths can be obtained by changing the elements andparameters of the launch system and/or load.

The powder load 124, typically, is a fine particle powdered substancesuch that the particle sizes or grain are less than 1000 microns indiameter, and preferably less than 500 microns, more preferably lessthan 250 microns, and in many instances less than 100 microns. It hasbeen found that the generally the smaller the particle diameter in apowdered load 124, the more effective the dispersal, and typically thelarger the volume of the dispersal, of the powder into a cloud uponbeing launched from the launch system 100. In some instances, the natureof the cloud produced is similar to, for example, a cloud that is formedwhen clapping erasers together, only generally much larger in volume. Aswill be seen, it is advantageous that the powder load 124 produce a finecloud of the powder such that the cloud will be dispersed on and aboutthe target, such that the target inhales the substance, and/or creates arelatively large suspended powder cloud barrier (e.g., larger than anadult human head, adult human torso or adult human body).

As described above, the powder load 124 can include an inhibitingsubstance, and in some instances comprises a powdered oleoresin capsicumpowder or capsaicin powder that has a particle size of less than 500microns, preferably less than 100 microns, and more preferably less than20 microns, e.g. 5 to 10 microns in diameter. Thus, when such powder israpidly launch from a launch system 100 a cloud of finely powderedsubstance 124 is produced that has a depth of at least about 6 feet, anda width of at least 2 feet and preferably at least 3 feet in diameter.This cloud advantageously “wafts” in the air for several seconds, forexample, more than 5 seconds and with some powder loads 124 more than 10seconds before settling, allowing sufficient time for a target to inhalethe powdered substance, and maintain a suspended powder barrier allowinga user to escape. Further, the amount of inhibiting substance and/orportion of inhibiting powder within the powder load 124 can varydepending on many factors. For example, the powder load 124 can containabout 5% PAVA (Capsaicin II, nonivamide) capsacinoids by weight, withabout 95% by weight of inert substances, such as barium sulfate and/orweighting substance(s).

Still referring to FIG. 1, the frame 110 and/or barrel assembly 112 canbe constructed of substantially any material or combinations ofmaterials that withstand the impulse and propulsion pressures induced bythe activation of the launch system 100. For example, the frame 110and/or barrel assembly 112 can be fabricated from any number ofmaterials such as, but not limited to, plastic, metal, metal alloysand/or other such similar materials or combinations of materials. Insome implementations, one or more components of the frame 110 and/orbarrel assembly 112 are formed from molded metal and/or plastic, such asinjection molded plastic and/or reinforced plastic (e.g., reinforcedwith metal, fiberglass or other reinforcement materials). Additionallyin some embodiments, the barrel 118 may be opaque or partially opaque sothat a user can verify that the powder load 124 has not been launched.

Further, as introduced above, the frame 110 and barrel assembly 112 canbe constructed to be detachable. This allows, in some embodiments, thebarrel assembly 112 to be pre-loaded with the pusher 126, powder load124 and seal 128. Similarly, the launch system 110 can be constructedsuch that the barrel is a replaceable and/or disposable portion that isreadily removed from the frame 110 allowing subsequent and/oralternative barrels 112 loaded with powder loads 124 to be easily, andtypically, rapidly attached replacing a barrel from which the powderload 124 had been launched, to replace a barrel that may have a defect,to replace a barrel having a first type of powder load with a barrelhaving a different type of powder load, and other such applications. Thebarrel 118 can be substantially any size that is capable of providingthe rapid expulsion of the loose powder load 124 while maintainingsufficient pressure within the barrel to provide the desired propulsionforce to launch the loose powder load at sufficient velocity to inducethe powder cloud. For example, in some instances, the barrel has alength that is less than 3 inches, and in some embodiments less than 2inches greater than a length of the pusher 126, powder load 124 and seal128 (e.g., in some embodiments, the length of the barrel 118 is lessthan 3 inches); and with a diameter that is between about 0.25 inches to2.0 inches, for example about 0.7 inches.

As described above, powder loads of the present embodiments, such aspowder load 124, can be launched using any number of different types ofimpulse energy sources. Again, the impulse energy source can be, forexample, from a launch system using the pressure impulse from aconventional firearm primer; an electrically fired primer; a burning gasgenerator common to automobile airbag technology; known gunpowdertechnology; by spark ignition of propane, butane or other hydrocarbons;sources of compressed gas such canisters or cartridges of compressed gas(e.g., such as found in refillable paintball gas cylinders); replaceablecompressed gas cartridges (e.g., cartridges such as used in air pistolsand inflation devices); and other such sources of impulse pressureand/or combinations of sources of impulse pressure.

In actuating the launch system 100, an actuator, such as a triggerbutton, lever, trigger or other such actuator, activated to release aspring mechanism, move a drive mechanism, actuate a valve, move alevered wedge mechanism or other such method to release the impulsepressure. In some embodiments that utilize compressed gas as at least aportion of the impulse pressure, the actuator causes a compressed gascartridge to be forces into contact with a puncture pin; a valve to beopened; or uses other release to affect a release of the compressed gasto be directed into the barrel 118 and propel the powder load 124 fromthe barrel 118 (or shell cartridge containing the powder loads in somealternative embodiments). The expanding gases released into the barrel118 launch the powder load 124 (or one or more various powder loadsdescribed below) towards the intended target. Alternatively oradditionally, in those embodiments that utilize a primer, gunpowderand/or chemical gas generator as the source of impulse pressure 114,then the actuator causes an ignition of the primer, gunpowder, chemicalgas generator, etc., which produces hot gases that cause an impulse ofexpanding gas to propel the powder load 124 from the barrel 118 (orcartridge shell).

FIG. 2 shows a simplified cross-sectional view of a launch system 200,similar to that of FIG. 1, with a membrane powder load 210 comprisingpowder 212 retained within a membrane 214. As introduced above, in someimplementations the powder load 212 is retained within a membrane orfilm prior to activation of the launch system 100. The membrane 214 istypically relatively thin and easily ruptured, and can be constructed ofsubstantially any relevant material or combinations of materials suchas, but not limited to, plastic, plastic wrap, paper, wax paper, foam,wax and/or other such similar materials or combinations of materials.Typically, the force applied by the pusher 126, in response to theimpulse pressure, against the membrane powder load 210 (as well as theforce of the membrane powder load 210 against the seal 128) readilybreaks the membrane 214 and the loose powder 212 is released from themembrane such that the loose powder 212 is in contact with the interiorsurface of the barrel 118 for a least a portion of the length of thebarrel 118 as the loose powder 212 travels along the barrel 118 towardthe exit end 120 of the barrel assembly 112 to be ejected from thebarrel assembly 112 in a loose, and in some instances an aerosol state.The broken membrane is relatively light and typically has very pooraerodynamics (particularly after being ruptured within the barrel 118),and as such rapidly falls to the ground and typically does not strikethe intended target.

Some embodiments include one or more tabs 224, knife edges, pins or thelike positioned within the barrel 118 or at the exit end 120 of thebarrel assembly 112. The one or more tabs 224 cut, snag or otherwiserupture the membrane as the membrane powder load 210 is propelled alongthe barrel 118. In some instance multiple tabs provide multiple cutsand/or effectively shred or partially shred the membrane 214.Additionally or alternatively, a bar or cross-bar structure (not shown)can be fixed within the barrel 118 or at the exit end 120 of the barrelto rupture the membrane 214. Still further, in some instances themembrane may be glued to the interior of the barrel, the interior or aportion of the interior of the barrel may rough or other such mechanismscan be used to rupture the membrane.

The barrel 118 of the launch system 200 depicted in FIG. 2 is shown witha length that is longer than the barrel of the launch system 100 ofFIG. 1. It is noted that the length of the barrel assembly 112 and/orbore 118 can vary depending on payload weight, desired dispersioneffect, amount of propulsion forces, launch distance and other suchfactors. The length of the barrel does not significantly alter thedispersion of the powder load 124 in generating a powder cloud, for atleast short or relatively short distances of less than about 15 feet.The longer barrel, however, may simplify assembly of varying powderlaunch loads and/or embodiments of the launch system as described below.

FIG. 3 depicts a simplified cross-sectional view of the launch system300, similar to the launch systems 100, 200 of FIGS. 1-2, with a powderload 310, according to some embodiments, comprising the membrane powderload 210, comprising powder 212 retained within a membrane 214, and aprojectile 320. In the embodiment shown in FIG. 3, the powder load 310is retained between a pusher 126 and a seal 128. In some embodiments,the seal 128 is not included and instead the projectile 320 provides aseal or at least a sufficient seal to launch the payloads. Additionallyor alternatively, an O-ring (not shown) or other similar structure canbe incorporated into the barrel 118 to retain the projectile 320 withinthe barrel assembly 112 and/or to establish at least a sufficientenvironmental seal between the O-ring and the projectile 320.

The projectile 320 includes a frangible shell 322 and a payload 324. Thepayload 324 can include a powdered payload that can be that same as,similar to or different from the powder load 124 and/or powder 212. Inother embodiments, the payload 324 is a liquid payload and/or acombination of liquid and powder. The projectile 320 and/or payload 324can be the same or similar to one or more of the projectiles and/orpayloads described in U.S. Pat. Nos. 7,194,960; 6,546,874; 6,393,992;and 5,965,839, and Patent Application Publication Nos. 2005/0188886; and2006/0027223, all of which are incorporated herein by reference in theirentirety.

Upon activation of the actuator of the launch system 300, the source ofimpulse pressure 114 delivers the propulsion force through the entryopening 116 and into the barrel 118 to drive the loose powder 212 andprojectile 320 from the launch system 300. Again, the membrane 214ruptures during launch, typically as a result of the propulsion pressureand/or the force exerted on either side of the membrane powder load 210by the pusher 126 and projectile 320. As described above with referenceto FIG. 2, one or more tabs 224 or other such structures can beincorporated into the barrel 118 or at the exit end 120 to ensure thatthe membrane 214 breaks prior to leaving the barrel 118.

The amount and/or weight of the powder load 310 can be substantially thesame as those described above. For example, the projectile 320 can havea weight of about 3 grams while the membrane powder load 210 can have aweight of about 2-3 grams, while employing a source of impulse pressure114 that is substantially the same as those for the embodiments depictedin FIGS. 1-2 and described above. It is noted, however, that the amountof propulsion force can vary depending on the size and/or weight of thepowder load 310, and in some instances the length of the barrel 118between the projectile 320 and the exit end 120. In some embodiments,the barrel 112 has a longer length when a projectile 320 is launchedfrom the launch system 300. The longer barrel length allows theprojectile 320 to gain sufficient velocity when launched to have adesired launch distance and/or provide a desired kinetic impact at thetarget (e.g., that results in pain to the target). Further in someimplementations, barrel 118 may include rifling that can induce rotationto the projectile 320, which in some implementations enhances stabilityand/or increases a launch distance.

FIG. 4 depicts a simplified cross-sectional view of the launch system400, similar to the launch systems 100, 200, 300 of FIGS. 1-3, with apowder load 410, according to some embodiments, comprising an unenclosedand free powder 412 and a projectile 320 positioned within the barrel118. The powder load 410 is retained between a pusher 126 and a seal128. In some embodiments, the seal 128 is not included and instead theprojectile 320 or projectile and sealing structure (e.g., O-ring),provides a seal or at least a sufficient seal to protect the loosepowder 412 from the environment. The powder 412 is a loose powder loadin that at least a majority of the powder 412 when ejected from thebarrel 118 is loose and unenclosed to rapidly disperse into the powdercloud extending from substantially the exit end 120 of the barrel 118 asdescribed above and further below. In some instances the powder 412 canbe tapped or lightly compressed while still being launched as loosepowder. Upon activation the powder load 410 is propelled from the barrel118 such that the projectile is launched while the powder 412 is ejectedas a loose powder establishing a powder cloud.

The amount and/or weight of the powder load 410 can be substantially thesame as those described above. For example, the projectile 320 can havea weight of about 3 grams while the powder load 412 can have a weight ofabout 2-3 grams, while employing a source of impulse pressure 114 thatis substantially the same as those for the embodiments depicted in FIGS.1-2 and described above. It is noted, however, that the amount ofpropulsion force can vary depending on the size and/or weight of thepowder load 410, and in some instances the length of the barrel 118between the projectile 320 and the exit end 120. In some embodiments,the barrel 112 has a longer length when a projectile 320 is launchedfrom the launch system 400. The longer barrel length allows theprojectile to gain sufficient velocity when launched to have a desiredlaunch distance and/or provide a desired kinetic impact at the target(e.g., that results in pain to the target). Further in someimplementations, barrel 118 may include rifling that can induce rotationto the projectile 320, which in some implementations enhances stabilityand/or increases a launch distance.

FIG. 5 depicts a simplified cross-sectional view of the launch system500, similar to the launch systems 100, 200 of FIGS. 1-2, with a powderload 510, according to some embodiments, comprising powder 512 and aprojectile 320 with a divider or separator 514 positioned between thepowder 512 and the projectile 320. The powder 512 is unbound andunencased other than by the interior of the barrel 118, the pusher 126and separator 514, and in some instances can be similar to the powders124, 412 of FIGS. 1 and 4. The powder 512 is a loose powder load in thatat least a majority of the powder 512 when ejected from the barrel 118is loose and unbounded to rapidly disperse into the powder cloudextending from substantially the exit end 120 of the barrel 118 asdescribed above and further below. The divider 514 retains the powder512 and substantially prevents the powder 512 from contacting theprojectile 320, which may in some instances avoid the powder 512 frombeing lodged between the shell 322 of the projectile 320 and theinterior surface of the barrel 118. In some instances, the lodging ofpowder 512 between the shell 322 of the projectile and the interiorsurface of the barrel 118 may jam the projectile within the barrel 118and/or result in requiring an increased propulsion pressure to launchthe powder load 510. The divider 514 can be constructed of substantiallyany number of materials such as, but not limited to, urethane foam,polymer foam, Styrofoam, paper, cardboard, plastic, rubber, wax,paraffin and/or other such similar materials or combinations ofmaterials. In some implementations, the divider 514 is similar to thepusher 126 and/or seal 128. Further, the divider can create a seal withthe interior of the barrel 118 and/or can be glued or otherwise securedwith the interior of the barrel.

The powder 512 can be substantially similar to the powder 124 of FIG. 1.The amount and/or weight of the powder 512 can, in some embodiments, bebetween about 2-3 grams when the projectile 320 has a weight of about 3grams. The weight of the powder 512 and/or project can vary depending onan amount of propulsion force that can be generated from the source ofimpulse pressure 114, and/or a desired launch distance of the projectile320. As described with regard to at least FIG. 3, the length of thebarrel assembly 112 can also be increased in some implementations toachieve a desired velocity of the projectile 320 at the exit end 120 ofthe barrel. Additionally or alternatively, the dimensions of the pusher126, divider 514 and/or seal 128 can also be adjusted.

FIG. 6 depicts a simplified cross-sectional view of a launch system 600according to some embodiments. The launch system 600 includes a frame610 and a barrel assembly 612. The frame 610 includes an actuator ortrigger mechanism 616 and a driver 618. The barrel assembly 612comprises a source of impulse pressure 620 and a barrel 622. Further,the source of impulse pressure 620 includes a compressed gas cartridge,cylinder or the like 624, a puncture pin 626, an expansion chamber 628and a burst diaphragm or disc 630. The barrel 622 includes an entryopening 632 and a barrel bore 634. A load is incorporated into thebarrel bore 634 and the load can include, in some implementations, apusher 640, powder payload 642 and a seal 644.

In some implementations the barrel assembly 612 is detachable from theframe 610, and further in some embodiments the barrel assembly 612 isreplaceable such that upon activation of the launch system 600 and thelaunching of the powder payload 642, the spent barrel assembly can bedetached and a new barrel assembly 612 can be secured with the frame610. Substantially any mechanism can be employed to secure the barrelassembly 612 with the frame 610. Some of these mechanisms can include,but are not limited to, screw threading, pin and groove, one or morespring loaded pins, latch(es) and other such methods.

FIG. 7 depicts a simplified cross-sectional view of the frame 610 of thelaunch system 600 of FIG. 6. The frame 610 as introduced above includesthe trigger mechanism 616 and the driver 618. Additionally, the frame610 includes a barrel assembly receiving port 710 that receives andsecures a barrel assembly 612. In some implementations, the triggermechanism further includes a trigger or actuator lever 712 that ispivotably secured with the frame 610 at a pivot 714, with a rivet,screw, pin or other such mechanism. Further, the lever 712 is in contactwith and/or secured with the driver 618. A driver stop 716 is alsoincluded in some implementations as described fully below.

FIG. 8 depicts a simplified cross-sectional view of the barrel assembly612, according to some embodiments, that can be utilized in the launchsystem 600 of FIG. 6. FIG. 9 depicts an enlarged view of a portion ofthe barrel assembly 612 of FIG. 8 showing the compressed gas cartridge624, the puncture pin 626, the expansion chamber 628, burst diaphragm630 and entry opening 632. Referring to FIGS. 6 and 8-9, in someembodiments the barrel assembly 612 is assembled from a cartridge holderor housing 812 and the barrel 622 that are secured together with theburst diaphragm 630 positioned proximate an interface between thecartridge holder 812 and the barrel 622. The cartridge holder 812, insome implementations, is secured with the barrel 622 through threading,gluing, tongue and groove, welding and other relevant methods, orcombinations of methods. For example, the cartridge holder 812 caninclude threading 814 to be screwed together with the barrel 622, and afurther adhesive or glue can be included, that in implementations may atleast partially melt the material of the cartridge holder and/or barrelto further secure, bond and/or partially weld the components together.Securing the cartridge holder 812 and barrel 622 maintains therelationship between the cartridge holder 812 and the barrel duringlaunching and can withstand the pressures generated in launching theloose powder load 642 and/or a projectile. In some implementations, forexample, the cartridge holder 812 and the barrel 622 can be secured byapplying glue (e.g., Instant Krazy Glue™) that can be brushed ontothreads 814 of one or both the cartridge holder 812 and the barrel 622.In some instances the burst diaphragm 630 is retained in position byclamping the burst diaphragm or a frame or ring positioned with and/orsecured with the burst diaphragm between the cartridge holder 812 andthe barrel 622. Alternatively, or additionally, the burst diaphragm 630is also glued or otherwise sealed in place. For example, a glue, such asLOCTITE Superflex Clear RTV™) can be applied on one or both sides of theburst diaphragm (e.g., on both sides of a perimeter of the burstdiaphragm 630 to help in preventing leaks). Additionally in someimplementations, the barrel assembly 612 is has a cylindrical structureto take advantage of the inherent structural strength to aid inwithstanding the launch pressures.

The compressed gas cartridge 624 is slidably positioned within acartridge port or chamber 912 of the barrel assembly 612 that allows thecompressed gas cartridge 624 to slide, when driven by the driver 618,from a first position separated from the puncture pin 626 to a secondposition in contact with and punctured by the puncture pin 626. In someimplementations a cartridge seal 914 is positioned within the cartridgeport 912 proximate the puncture pin 626. The compressed gas cartridge624 transitions from a first position when driven by the driver 618 to asecond position to be punctured by the puncture pin 626. Typically, thecompressed gas cartridge 624 is further in contact with the cartridgeseal 914 that establishes a seal relative to the compressed gascartridge and the puncture pin such that substantially all of thereleased gas is directed into the expansion chamber 628, either throughand/or around the puncture pin 626. The cartridge seal 914 can beconfigured from substantially any relevant mechanism, such as an O-ring,washer or other such mechanism, and similarly can be constructed ofsubstantially any relevant material to establish the desired seal. Insome implementations, the cartridge seal 914 is part of a puncture pinassembly that further contains the puncture pin 626 and allows thepuncture pin to be secured within the barrel assembly 612 relative tothe cartridge seal 912. It is noted that the launch system 600 is shownsuch that the driver 618 drives the compressed gas cartridge 624 ontothe puncture pin 626. In other embodiments, however, the puncture pin626 can be driven into the compressed gas cartridge 624 to puncture thecartridge and release the gas, or both can be driven toward the other.

A passage, conduit or other such tube 916 can be included in someimplementations that extends between the puncture pin 626 and theexpansion chamber 628 to carry the gas released from the compressed gascartridge 624 into the expansion chamber 628. The released gas from thecompressed gas cartridge can flow through and/or around the puncture pin626 and into the expansion chamber.

The burst diaphragm630 seals the expansion chamber 628 from the entryopening 632 and the barrel bore 634. As compressed gas continues to bereleased from the compressed gas cartridge 624, pressure builds withinthe expansion chamber 628 and against the burst diaphragm 630. When thepressure within the expansion chamber 628 exceeds a burst threshold ofthe burst diaphragm, the burst diaphragm bursts or ruptures rapidlyreleasing the gas from the expansion chamber 628, through the entryopening 632 and into the barrel bore 634. The cross-sectional areas ofthe burst diagraph 630 and entry opening 632 are relatively largecompared with the size of the puncture hole in the cartridge resultingfrom being punctured by the puncture pin. Further, the burst openingthat results within the burst diaphragm as a result of bursting is alsorelatively large compared to the puncture hole, and in some instances isabout the size of the entry opening 116 (e.g., in those instances wherethe burst diaphragm ruptures into the entry opening 116). In someimplementations, the area of the burst opening and/or entry opening 116is 5, 10 or more times the size of the puncture hole. Because of therelatively large size of the burst opening through which the compressedgas is released into the barrel bore 634, a relatively large amount ofcompressed gas is rapidly released into the barrel bore 634 to provide agreater propulsion pressure onto the pusher 640 and powder load 642 thanotherwise would be provided from the puncture hole alone. The rapidlyexplosive rupturing of the burst diaphragm provides the relatively largeopening to effect the rapid release of the propulsion force. The launchsystem can be configured such that a size of a resulting burst openingis established or tuned depending desired cloud dimensions, a loadweight, burst diaphragm material and/or thickness, an amount ofpropulsion pressure, an expected amount of impulse pressure and/or othersuch factors. Additionally, in some implementations the rupture of theburst diaphragm results in an audible noise, report, retort andtypically a relatively loud pop or bang (typically that can be heard bya human at more than 15 feet away, generally at more than 20 feet awayand in some instances more than 30 feet away), that can startle atarget, may notify others individuals in the area of the threat, and insome instance induces a reaction by the target, such as taking aninvoluntary breath that can cause the target to breath in some of theinhibiting powder of the powder cloud 1210.

The size and/or volume of the expansion chamber 628 typically depends onthe compressed gas stored within the compressed gas cartridge 624, thevolume of the compressed gas cartridge 624, a burst threshold of theburst diaphragm or a combination of one or more of these. For example,when the compressed gas cartridge 624 stores liquid carbon dioxide(CO₂), the volume of the expansion chamber 628 is typically configuredto be equal to or larger than the volume of the compressed gas cartridge624. This is due, at least, to the fact that as the carbon dioxidebottled in liquid form is released there is a phase transition as theliquid transitions and expands into a gaseous state. In someimplementations, the volume of the expansion chamber 628 is greater thattwice the volume of the compressed gas cartridge 624. For example insome embodiments, the volume of the compressed gas cartridge is about0.1 cubic inches, while the volume of expansion chamber 628 is about 0.5cubic inches, providing about a 5-to-1 amplification of the volume withthe use of the expansion chamber 628 in cooperation with the burstdiaphragm 630. As another example, the volume of the expansion chamber628 can be about 0.09 cubic inches, which can comprise two connectedcylinders, one that is about 0.382 inch in diameter and about 0.417inches long, and the other that is about 0.627 inch in diameter andabout 0.133 inches long. Other sources of compressed gas and/or types ofgas can be utilized as introduced above, such as air, nitrogen, otherrelevant gases or combinations of gases. The expansion chamber 628and/or burst diaphragm 630 can be configured, selected and/or otherwisetuned to one or more desired performance characteristics, such as butnot limited to desired cloud dimensions, a powder load weight, an amountof propulsion pressure, an expected amount of impulse pressure, burstdiaphragm material and/or thickness, and/or other such factors.

The burst diaphragm 630 can be constructed of substantially any relevantmaterial capable of withstanding the desired pressures and rupturing atabout a desired pressure threshold. Further, the burst diaphragm 630, insome embodiments, is a replaceable, disposable rupture disk membranesecured between the barrel bore 634 and the expansion chamber 628. Whenthe gas pressure in the expansion chamber volume reaches the stresslimits of the membrane material of the burst diaphragm, the burstdiaphragm ruptures and the expanded gas is released to accelerate thepowder load 642 (and/or one or more projectiles) out of barrel bore 634.The burst diaphragm 630 can be constructed of Mylar™, polyethyleneterephthalate (PET) Polyester film, paper, plastics, metal, andsubstantially any other relevant material that maintains the expandinggas within the expansion chamber allowing gas pressure to build until apredefined and/or desired pressure is attained at which point the burstdisk ruptures. For example, in some implementations the burst diaphragm630 can be made of Mylar™ with a thickness of more than 1.5 mm, forexample, 3 mm, or other such thickness to provide a burst threshold at adesired level, and/or include structural weakening features.

The burst diaphragm 630 may rupture by exceeding the stress limit of thematerial, alternatively by coming in contact with a sharp device withinthe barrel assembly 612 that causes the burst diaphragm to puncturereleasing the built-up gas, and/or by breaking a seal or other means ofrupturing the burst diaphragm. The burst diaphragm 630, in someimplementations, is scored to control or change the pressure at whichthe burst diaphragm bursts. The scoring can be in substantially anyconfiguration to establish weakening points that allow, in someimplementations, more precise and consistent bursting at desiredpressure thresholds. Additionally and/or alternatively, the burstdiaphragm 630 under pressure may be designed to burst using othermethods such as: mechanical cutting or piercing of the burst diaphragm;using heated coils or electrical arcs to create or melt a weak sectionor an initial pin or small hole in the burst diaphragm; or other methodsof aiding rupturing the diaphragm material. Typically, the burstdiaphragms have consistent burst thresholds providing consistentoperation of the launch system 600 between launches (e.g., by replacinga spent barrel assembly 612 with a new, loaded barrel assembly). Otherembodiments of the launch system 600 may employ one or more of amechanical valve that opens; a fixed diaphragm that opens by moving,folding and the like without rupture (e.g., using magnets that releaseat defined pressures); a friction held or other types of gas plug;and/or other relevant types of gas retainer design methods that can bemade to move or open to allow gas flow. The burst diaphragm 630, valveand/or gas plug at least in part allows sufficient gas pressure andvolume to buildup, and once the burst diaphragm ruptures (or isotherwise released) the gas enters the barrel bore 634 providing apropulsion force on the pusher 640 to propel the powder load 642 fromthe barrel bore 634 creating the desired powder cloud.

Referring back to FIGS. 6-7, the driver 618 can be substantially anymechanism that responds to the actuation lever 712 to drive thecompressed gas cartridge 624 onto the puncture pin 626, or that drivesthe puncture pin into the compressed gas cartridge. In someimplementations, the driver 618 transfers the motion of the actuationlever 712 to the compressed gas cartridge 624 or puncture pin 626. Forexample, as the lever 712 is actuated by an external force (representedby the arrow labeled 720) the lever pivots at the pivot 714 andactivates the driver 618 to move the compressed gas cartridge 624 to bepunctured by the puncture pin 626. In some embodiments, the frame 610further includes a driver stop 716. The driver stop is cooperated withthe driver 618 to maintain a positioning of the driver 618, at leastprior to activation.

FIGS. 10-11 show a simplified front view and a side view, respectively,of a driver 1010 that can be employed for the driver 618 of the launchsystem 600 of FIGS. 6-7. The driver 1010 includes a fixed fulcrum armpair 1012 and a lever fulcrum arm 1014. As shown in FIG. 11, the fixedfulcrum arm pair 1012 can include two fulcrum arms 1020-1021 that arepositioned on either side of the lever fulcrum arm 1014. It will beapparent to those skilled in the art that other configurations can beutilized. For example, the fixed fulcrum arm pair 1012 or lever fulcrumarm 1014 can be replaced by a single, generally Y-shaped fulcrum arm.The fixed fulcrum arm pair 1012 is secured with the frame 610 at a firstpivot 1024, and pivots relative to the frame 610 at the pivot 1024.Further, the fixed fulcrum arm pair 1012 is secured with the leverfulcrum arm 1014 at a second pivot 1026. Similarly, the lever fulcrumarm 1014 is pivotably secured with the actuator lever 712 at a thirdpivot 1028.

Upon activation of the actuation lever 712, the lever fulcrum arm 1014is moved toward the fixed fulcrum arm pair 1012. As the lever fulcrumarm 1014 is moved toward the fixed fulcrum arm pair 1012 both the leverfulcrum arm 1014 and the fixed fulcrum arm pair 1012 move, at the secondpivot 1026, generally laterally and/or perpendicular to the forceapplied by the lever fulcrum arm at pivot 1028. This lateral movement ofthe lever fulcrum arm 1014 and the fixed fulcrum arm pair 1012 resultsin a relatively large lateral movement for a relatively small verticalmotion.

As introduced above, some embodiments include a driver stop 716. Thedriver stop 716 can maintain a positioning of the lever fulcrum arm 1014relative to the fixed fulcrum arm pair 1012. Particularly, the driverstop 716 prevents the lever fulcrum arm 1014 from being aligned with thefixed fulcrum arm pair 1012, and maintains an angle 1030 between thelever fulcrum arm 1014 and the fixed fulcrum arm pair 1012. This angle1030 ensures that the driver 618 will bend at the second pivot 1026 andinduce the lateral motion to drive the compressed gas cartridge 624 ontothe puncture pin 626 (or the puncture pin into the compressed gascartridge). In some implementations, the actuation lever 712 incooperation with the driver 618 can induce 40 lbs or more of pressurethat can be exerted on the compressed gas cartridge 624 to puncture thecartridge.

As described above, the launch systems 100, 600 rapidly launch loosepowder, e.g., loose powder 124 (and in some instances a projectile,e.g., projectile 320) generating a powder cloud. FIG. 12 depicts asimplified block diagram representation of a powder cloud 1210 generatedfollowing the activation, by a user 1214, of a launch system 1212 (whichcan be similar, for example, to the launch systems 100, 600 of FIGS.1-9) directed at a target 1216. The use of the expansion chamber 628 andthe burst diaphragm 630 allows the launch system 1212 to rapidly applythe propulsion pressure to the pusher 126, 640. As described above, theburst diaphragm 630 fails at a burst threshold providing a relativelylarge hole through which the compress gas rapidly, and in some instancessubstantially instantaneously exits. The built up pressure within theexpansion chamber 628 can be substantially any relevant pressure toachieve the desired propulsion pressure. In some implementations, burstthreshold can be 600 psi or more. For example, when using compressed gascartridge 624 holding compressed carbon dioxide at about 800 psi, theburst diaphragm 630 can be selected to have a rupture threshold of lessthan 800 psi, and the expansion chamber can be configured with a volumethat allows the compressed carbon dioxide to be released from thecompressed gas cartridge 624, phase transition to the gaseous state, andgenerate a sufficient pressure within the expansion chamber 628 andagainst the burst diaphragm 630 to rupture the burst diaphragm providinga rapid release of the gas to drive the pusher 640 to propelsubstantially all, and preferably, the entire power load 642 from thebarrel 622. As a result, the loose powder 642 is launched from thebarrel 622 in less than one second, typically less than one half asecond, and more typically in less than hundreds of milliseconds fromthe time the compressed gas cartridge 624 is punctured.

Further, the propulsion pressure when released from the expansionchamber 628 is sufficient to launch the loose powder load 642 at asufficient velocity to generate the cloud 1210 of powder (which in someembodiments as described above, include inhibiting powder) establishinga barrier between the user 1214 and the target 1216. Further, the rapidlaunch of the loose powder load 642 results in the rapid dispersion ofthe powder cloud 1210 that has a depth 1218, measured from a exit end ofthe barrel at the time of launch and an advancing front end 1220 of thecloud, within less than a second, typically less than one half a second,and some implementations within less than tens of milliseconds from thetime the compressed gas cartridge 624 is punctured. For example, someembodiments establish an propulsion pressure of between about 600 and800 psi resulting in a rupture of the burst diaphragm 630 and propel theloose powder 642 from the launcher 610 at a velocity of greater than 100feet per second, typically greater than 200 feet per second, and in someinstance at about 300 feet per second or more, to produce a powder cloud1210 that has a depth 1218 (measured generally parallel with the lengthof the barrel 622 at the time of launch) of more than 5 feet, andtypically more than 8 feet, and in some instances as much as 14 feet ormore, in less than one half a second from the time the compressed gascartridge 624 is punctured; additionally, the loose powder 642 exits theexit end 120 of the barrel 622 at an angle 1222 relative to an axis ofthe barrel length that is generally greater than about 10 degrees, andin some instances greater than 20 degrees such that a width of thepowder cloud 1210 is greater than about 2 feet, and typically greaterthan about 3 feet when measured at a depth 1220 of at least 8 feet. Thelaunch system can be configured and/or tuned to achieve a desired exitvelocity depending on one or combinations of the many variables, such asbut not limited to, source gas pressure and volume, expansion chamberand volume, burst disk material and thickness, entry opening and/orburst diaphragm retaining ring hole, barrel length, payload weight andother such factors and/or combinations of factors.

As the powder cloud 1210 advances it envelops the target 1216 in thoseinstances where the target 1216 is within at least the depth range ofthe powder cloud and/or should the target try to advance toward the user1214. The inhibiting powder within the powder cloud 1210 rapidlycontacts and affects the target 1216 inhibiting and in some instanceseffectively disabling the target 1216. Further, because the launchsystems 100, 600 launch the loose powder load 124, 642 that generatesthe large powder cloud 1210, that is typically about as large as orlarger than an average adult human, the user 1214 is not required tohave good aim or directly hit the target 1216 with a projectile andstill achieve effective deterrent results. Instead, the powder cloud1210 establishes a barrier between the user and the target 1216 and insome instances surrounds and/or envelopes the target 1216. This powdercloud 1210 further “wafts” in the air for several seconds, for example,for more than 6 seconds and in some instances as much as 10 seconds ormore before settling, allowing sufficient time for the target 1216 toinhale the powdered substance and/or get irritant powder in the target'seyes, as well as allow the user 1214 sufficient time to flee with thebarrier of the powder cloud 1210 protecting the user's retreat.

This is in contrast to many non-lethal deterrent systems in that manynon-lethal deterrent systems require the user to be directly hit with aprojectile or stream of liquid. Further, some deterrent systems, such ascanisters of pepper spay, additionally require relatively long periodsof time of, in some instances, 10 seconds or more to empty the canisterof the inhibiting substance. Still further, many deterrent systems notonly require a direct hit of the target but further require theinhibiting substance to be a directed stream into the targets eyes,which can be particularly difficult in stressful situations where anassailant is rapidly approaching and trying to prevent the inhibitingsubstance from hitting his/her eyes.

The rapidly dispersed powder cloud 1210 does not require a direct hit ofa projectile or require that the powder be specifically directed intothe target's eyes. Instead, the powder envelops the target 1216 andenters the target's eyes (even passing around glasses), mouth and nasalcavity to inhibit the target 1216. Further, the powder cloud can passaround and/or through barriers to content a target, including passingaround obstacles that a target might be hiding behind, passing aroundglasses and other obstacles, obstructions and/or barriers.

Some embodiments, as described above can additionally include aprojectile 320. These embodiments additionally allow the user to launchthat projectile 320, which will typically travel a further distance thatthe powder cloud 1210. Additionally, the impact of the projectile 320provides a kinetic impact on the target that can result in pain to thetarget.

The powder loads 124, 624 and/or payload 324 of a projectile 320, asdescribed above, can comprise any of the following substances: aninhibiting substance such as oleoresin capsicum (also referred to as“OC”), capsaicin, nonivamide (i.e., one or more of the hottest activeingredients or capsaicinoids within oleoresin capsicum), tear gas (e.g.,CS or CN), PAVA and other such natural and synthetic inhibitingsubstances; a marking or tagging substance, such as a colored dye, UVdye, IR dye or other such marking substance; a malodorant; and/or aninert substance, such as barium sulfate, baby powder, corn starch,talcum or other such inert substances; weighting substances; and/or anycombination thereof. For example, the powder 124, 624 and/or payload 324in accordance with some embodiments can include a combination ofoleoresin capsicum and barium sulfate (or alternatively, a combinationof PAVA (nonivamide) and barium sulfate and/or other such inert powdersand/or weighting particles), at a desired ratio(s). Alternatively, acombination of PAVA and/or oleoresin capsicum, and/or other inhibitingsubstance, and a colored dye, malodorant and/or other marking substance,may be employed to simultaneously incapacitate the target and mark thetarget for later identification. In some embodiments a markingsubstance, a chemical marker or chemical fingerprinted paint, such asproduced by Yellow Jacket, Inc. of California, can be used whicheffectively leaves a chemical ID or chemical fingerprint on the target,which can be used by the police to verify a person was struck by anon-lethal projectile. As such, the chemical marker can include achemical ID, identifying the batch of the marker, that is formulatedinto the marker during manufacture. For example, a fleck of the chemicalmarker found on a suspect two weeks after being impacted with thechemical marker, can be chemically identified and traced to launchsystem 100; thus, the suspect may be linked to a crime scene by thechemical marker. In yet other alternatives, it may be desirable toemploy only a marking substance or only an inert substance, such asbarium sulfate or talcum, as the powder load 124, such as when thelaunch system 100, 600 is being used for training purposes. Similarly,any projectile 320 can be filled with an inhibiting powder or liquid,inert powder or liquid, and/or could be empty.

In some embodiments, the projectile 320 includes the shell 322, forexample, a spherical capsule (although other shapes of projectile bodiesmay be used) separable into two about equal halves (e.g. a first partand a second part), wherein the halves contain a powdered impairingsubstance sufficient in amount so that the shell 322 is about or greaterthan 50% full and preferably between about 60% and 99% full, forexample, from between 75% and 95%, for example, about 90% filled with apowdered substance 324 and wherein, to facilitate manufacture of theprojectile 320, the powdered substance 324 within each half iscompressed into a ball, tablet, mount and placed in one half and sealedwith the other half. Alternatively, the powder(s) 324 could becompressed into each separate half and retained therein by a thinmembrane, for example a paper foil, which contacts the inhibitingsubstance during assembly of the projectile 320. In this embodiment, thethin membrane is sufficiently strong to retain the desired substance 324within the shell 322 as it is manufactured or assembled, yet frangibleenough to readily rupture subsequent to sealing of the shell 322 andprior to, or at least simultaneously with, impact with the target.

The powder load 124 and/or payload 324 of the projectile 320 may, forexample, contain at least 0.5% inhibiting substances (such as PAVA,nonivamide (from natural or pharmaceutically and/or syntheticallyproduced sources) or oleoresin capsicum), e.g., between 1% and 30%,e.g., between 5% and 20%, with a remainder of the powder load 124 (orpayload 324) being either an inert substance or a marking substance or adifferent inhibiting substance, such as tear gas powder or a powdermalodorant. Alternatively, the powder load 124 and/or payload 324 may,for example, comprise at least 0.1% capsaicin (which is an activeingredient within oleoresin capsicum in either natural form orpharmaceutical produced form), and preferably at least 0.5% capsaicinwith the remainder of the powder load 124 and/or payload 324 as either amarking substance, an inert substance, and/or a malodorant. Similarly,more than one inhibiting substance may be combined to provide a total ofat least 0.1% to about 30% or more of inhibiting substances (e.g.,depending on the target to be impacted, such as a higher percentage maybe employed for impacting large animals).

In some variations, the powder load 124 and/or payload 324 may includefragments of solid material to enhance dispersion of the loose powderload 124 and/or payload 324. For example, crushed walnut shells, rice,wood shavings, metal particles, such as metal powder or metal particles,or the like may be added to the powder to help carry the powder awayfrom the launch system 100 and/or a point of rupture of the projectile320 against a target. The solid material, having a greater density andmass than the powder load 124 (e.g., of inhibiting substance, inertsubstance and/or marking substance) tends to project further from thelaunch system 100, thereby facilitating dispersion of the loose powderload 124 as it is carried by the solid material.

In further variations, a visible marking agent, a covert UV or IRvisible dye, malodorant, or other taggant can be added to the powderload 124 and/or payload 324 of the projectile 320 in order to provide amechanism for identifying the target at a later time. This feature ofthis variation may be particularly useful in law enforcement or militaryapplications, where evidence gathering may be enhanced if the target canbe marked. By combining a marking agent with an inhibiting substance asignificant synergism is achieved. In another aspect, marking can beeffected by bruising of the target due to the kinetic impact of theprojectile 320 against the target.

In some embodiments of a marking substance, the projectile shell 322,e.g., capsule, may contain a chemical compound that has a particularlyoffensive odor, also referred to as a malodorant. In use, the projectile320 can be launched at a suspect, such that the suspect will have anunwelcome odor on his or her person. Such odor will effectively “mark”the person. Additionally, a projectile 320 containing a malodorant as atleast part of the payload 324 may be used to repel or keep persons awayfrom a particular area. An area impacted by one or more projectiles 320will typically smell so offensive that it will keep others from comingnear the smell. The malodorant has applications in crowd dispersal andcrowd control, as well. On example of a malodorant that has aparticularly offensive odor is called “Dragons Breath” which is anorganic sulfur compound produced by DeNovo Industries, of The Woodlands,Tex. In variations of this embodiment, a projectile 320 can include asthe payload 320, or at least part of the payload, a glass capsulecontained within the projectile shell 322. The glass capsule sealswithin itself certain malodorants, such as Dragons Breath and/or othersulfur compounds, that have solvent properties that can eat through aplastic variety projectile shell. The glass capsule within theprojectile body is ruptured upon impact of the projectile body,releasing the malodorant. In further variations, the glass capsule isguided centrally within the projectile with protrusions formed withinthe projectile. These protrusions center the glass capsule within theprojectile capsule and additionally may provide pressure points toassist in the fracturing of the glass capsule upon impact.

In yet a further variation, the payload 324 within the projectile 320can include a powdered inhibiting substance combined with a liquid orgas irritant, or other agent to be delivered. The liquid or gas, and thepowdered irritant can be carried in separate chambers, in for example,separate halves of the projectile 320 using membranes described hereinto contain the powdered inhibiting substance and the other agent,keeping them separated, if needed. If a liquid or gas is contained byone or both of the membranes, such membranes can be made, for exampleout of plastic, vinyl, rubber or the like. The projectile 320 can besimilar to those described at least in U.S. Pat. Nos. 7,194,960;6,546,874; 6,393,992; and 5,965,839, and Patent Application PublicationNos. 2005/0188886, and 2006/0027223, all of which are incorporatedherein by reference in their entirety.

FIGS. 13 and 14 depict a side view and a cross-sectional view,respectively, of a launch system 1300 according to some embodiments. Thelaunch system 1300 includes a frame 1310 and a barrel assembly 1312.FIG. 15 depicts a side view of the frame 1310 of the launch system 1300of FIGS. 13-14. Referring to FIGS. 13-15, the launch system 1300 furtherincludes a safety 1314, an actuator or trigger lever 1316, a driver1418, a driver stop 1414, and an actuator lever biasing member 1416fixed with the frame 1310. The barrel assembly comprises a source ofimpulse pressure 1420 and a barrel 1422. Further, the source of impulsepressure 1420 comprises a compressed gas cartridge 1424, a puncture pin1426, an expansion chamber 1428 and a burst diaphragm 1430. The barrel622 includes an entry opening 1432 and a barrel bore 1434. A load isincorporated into the barrel bore 1434 and the load can include, in someimplementations, a pusher 1440, powder payload 1442 and a seal 1444.

The safety 1314 is slidably secured with the actuator lever 1316 andextends, when in an active state to prevent activation of the launchsystem 1300, through a hole 1326 of the frame 1310. In operation, a userwould slide the safety 1314 in a direction away from the exit end 1436of the barrel 1434, for example, by press the extended portion of thesafety 1314 that extends through the hole 1326 of the frame 1310. Theactuator lever 1316 is further cooperated with the lever biasing member1416 that biases the actuator lever 1316 away from the frame 1310. Upondepression of the actuator lever 1316, the lever biasing member 1416compresses, the actuator lever 1316 drives the driver 1418 into thecompressed gas cartridge 1426 to force the compressed gas cartridge ontothe puncture pin 1426. The punctured compressed gas cartridge 1424releases compressed gas through and/or around the puncture pin 1426 toenter the expansion chamber 1428. In some implementations the expansionchamber 1428 comprises two cooperated sub-chambers (which in someinstances are connecting cylinders) 1450, 1452. For example, the volumeof the expansion chamber 628 can be about 0.1 cubic inches, where thefirst cylindrical sub-chamber 1450 can have a diameter that is about 0.4inch and about 0.42 inches deep, and the second cylindrical sub-chamber1452 can have a diameter of about 0.63 inch and a depth of about 0.14inches.

Once the pressure within the expansion chamber exceeds a burst thresholdof the burst diaphragm 1430, the propulsion pressure rapidly enters thebarrel bore 1434 to drive the pusher 1440 that in turn drives the powder1442 from the barrel 1422. Some embodiments may further include a site1330 and/or laser site (not shown, but may be activated, for exampleupon disengaging the safety 1314) to aid the user in aiming the launchsystem 1300. Additionally, some embodiments may include a key ring 1332,clip or other fastener on which keys or other devices can be securedand/or that can provide for easy of carrying.

FIG. 16 depicts a simplified flow diagram of a process 1600 ofassembling a launch system, such as the launch system 600 or 1300 ofFIGS. 6-9 and 13-15, respectively. In step 1610 the driver 1418 ispositioned and secured within a first half of the frame 1310. In step1612, a safety 1314 and spring 1416 are secured with the actuator lever1316. In step 1614, the actuator lever 1316 is positioned and pivotablysecured with the frame and the driver 1418, such that the spring 1416cooperates with the frame 1310. In step 1616, a second half of the frameis secured with the first half of the frame to maintain a positioning ofthe actuator lever 1316 and driver 1418. In step 1618, a driver stop1414 is positioned within the frame 1310 to prevent the fixed fulcrumarm pair 1012 and a lever fulcrum arm 1014 from being aligned andmaintaining an angle between the fixed fulcrum arm pair 1012 and a leverfulcrum arm 1014.

In step 1620 a puncture pin assembly, comprising the puncture pin 1426,a cartridge seal 914 and gas passage or tube 916 are cooperated. In step1622 the puncture pin assembly is secured within the cartridge holder orhousing 812. In step 1624 a burst diaphragm or disc 1430 is positionedrelative to the expansion chamber 1428 formed in the cartridge holder812. In some embodiments the burst diaphragm 1428 is glued or otherwisesecured and/or sealed with the cartridge holder 812. In step 1626 abarrel 1422 is secured with the cartridge holder 812, for examplescrewed to the cartridge holder 812, with the entry opening 1432 beingpositioned adjacent the burst diaphragm 1428. Again, in someembodiments, the burst diaphragm 1428 is glued or otherwise securedand/or sealed with the barrel 1422. Similarly in some implementations,the barrel is a further glued with the cartridge holder 812.

In step 1630, a pusher 1440 is positioned within the barrel bore 1434adjacent the entry opening 1432. In step 1632, the powder load 1442 ispositioned within the barrel bore 1434 adjacent the pusher 1440. In step1634, a seal 1444 is secured within the barrel bore 1434 adjacent thepowder load 1442 sandwiching the unenclosed powder load between thepusher 1440 and the seal 1444. Typically, the seal 1444 is inserted intothe barrel bore 1434 to a depth that will keep the powder load sealed inthe barrel. Additionally, the seal can further be glued or otherwisesealed with the interior of the barrel bore in some embodiments. In step1636 a compressed gas cartridge 1424 is inserted into the cartridgeholder 812 adjacent the cartridge seal 914 and the puncture pin 1426. Insome implementations, the assembled frame 1310 and the barrel assembly1312 can be distributed separately. In other embodiments, an additionalstep 1638 can be implemented where the frame 1310 and the barrelassembly 1312 are detachably secured to each other prior todistribution.

FIG. 17 depicts a simplified flow diagram of a process 1700 ofactivating a launch system, such as one of launch systems 600 and 1300of FIGS. 6-9 and 13-15, respectively. In step 1710, the safety 1314,when present, is disengaged. In step 1712 the launch system 1300 isgenerally aimed at a target. In step 1714 the actuator lever 1316 iscompressed, depressed, squeezed or otherwise activated launching theload and producing a large volume, visible cloud that can potentiallyinhibit a target and/or provide a temporary inhibiting barrier. In someembodiments, the process 1700 further includes step 1716, where thespent barrel assembly is removed from the frame 1310 and a new barrelassembly 1312 is secured with the frame 1310. The process can terminatefollowing one of steps 1714 or 1716, or can return to step 1712 to againgenerally aim the launch system for the deployment of a subsequentpowder cloud 1210 to produce an additional powder cloud, effectivelyenlarging an inhibiting barrier and/or adding to the previous cloud. Asa result, the process in some implementations activates, in response toan actuation, a source of impulse pressure, launches loose powder from alaunch system, and generates a powder cloud comprising the loose powderthat has dimensions larger than a human torso. Typically, the loosepowder launched comprises inhibiting powder such that the powder cloudcomprises an inhibiting powder cloud.

For several decades, law enforcement agencies have used variousnon-lethal weapons to gain control of suspects, quell riots, savehostages, etc. Most of these non-lethal deployments utilize a ratherlarge launcher platform such as a shotgun, rifle or pistol to deploy theprojectiles. Further, to date, other than pepper spray, the generalpublic has not had access to a simple, low cost, non-lethal launcherthat could be easily carried and used for personal defense at home, inthe car or when on foot. The present embodiments provide low cost,compact non-lethal personal defense launch systems that can be quicklydeployed and are effective on human and animal targets.

Many conventional launch systems utilize a projectile to affect thetarget. For example, U.S. Pat. Nos. 7,194,960, 6,546,874, 6,393,992, and5,965,839, incorporated herein by reference in their entirety, describemany embodiments of frangible irritant powder filled projectiles, andsystems to launch such projectiles, that can affect targets utilizingirritant powder clouds. These projectiles can be employed, as describedabove, in some present embodiments.

Further, the present embodiments series of non-lethal powder loads thatcan be launched by many different types of propulsion force or pressure,and from many types of launchers, to be used against a target, such as athreatening human or animal. Some of the launch systems are that can beused to launch the loose powder loads are described here. However, otherlaunchers may be used, in some implementations. One or more such compactlaunch device that could be utilized to launch the loose orprojectile-less irritant powder loads described herein include one ormore of the launching devices described in co-pending U.S. patentapplication Ser. No. 11/129,230, filed May 12, 2005, to Vasel et al.,and entitled COMPACT PROJECTILE LAUNCHER.

At least some embodiments of the launch systems described herein easilyfit in a person's hand, a purse, pocket, glove box, and the like, andare capable of launching the loose powder loads of powder irritants,inert substances and/or marking substances. Further, these launchsystems expel a cloud of irritant powder towards a target, for example,as a non-lethal defense. This irritant powder cloud typically has adistracting, incapacitating and/or repelling effect on the target, be ita human or animal, and in some instances is visible to a target furtherinhibiting the target. The irritant and distraction effects on thetarget may allow the user to retreat to a safer location, get away froman attacker, or if used by law enforcement or security personnel, subduean individual for arrest. The propulsion force or pressure used tolaunch the loose powder can include, but are not limited to, compressedgas, firearm primers, gunpowder, burning hydrocarbons, chemical gasgenerators or other means to accelerate these non-lethal irritant powderloads towards the intended target(s). The innovative chemical loadsdescribed herein can be directly loaded in barrels attached to thesemany launch devices or loaded into cartridge shells that can be utilizedin these or other types of launchers.

While the invention herein disclosed has been described by means ofspecific embodiments and applications thereof, numerous modificationsand variations could be made thereto by those skilled in the art withoutdeparting from the scope of the invention set forth in the claims.

1. A launch system comprising: a frame; a source of impulse pressurecooperated with the frame; a barrel secured relative to the frame andcooperated with the source of impulse pressure to receive a propellantpressure from the source of impulse pressure; a particulate loadpositioned within an interior of the barrel; and a burst diaphragmsecured between the source of the impulse pressure and the particulateload, wherein the burst diaphragm retains the impulse pressure from thesource of impulse pressure until a pressure of about equal to a burstthreshold of the burst diaphragm such that the burst diaphragm burstsreleasing the propellant pressure into the barrel to force theparticulate load out of the barrel.
 2. The launch system according toclaim 1, further comprising: an actuator cooperated with the source ofimpulse pressure, such that upon activation of the actuator the sourceof impulse pressure releases the impulse pressure and the bursting ofthe burst diaphragm in response to impulse pressure instantaneouslylaunches substantially all of the particulate load in response to asingle actuation of the actuator.
 3. The launch system according toclaim 1, wherein the source of impulse pressure comprises: a compressedgas cartridge storing compressed gas; a puncture pin positioned relativeto the compressed gas cartridge; and an expansion chamber positionedbetween said compressed gas cartridge and said burst diaphragm; whereinsaid burst diaphragm is positioned between the expansion chamber and theparticulate load, such that upon the activation; one of the puncture pinand compressed gas cartridge is moved relative to the other such thatthe puncture pin punctures the compressed gas cartridge releasing thecompressed gas into the expansion chamber, resulting in the increasingpressure applied to the burst diaphragm to burst the burst diaphragm,releasing the compressed gas to expel the particulate load from thebarrel.
 4. The launch system according to claim 3, wherein saidcompressed gas cartridge contains carbon dioxide which is stored underpressure in a substantially liquid form which is then sublimated to agaseous form when released to build up substantial pressure in saidexpansion chamber before accelerating the particulate load.
 5. Thelaunch system according to claim 4, wherein said expansion chamberworking in conjunction with said burst diaphragm allows released gasfrom said compressed gas cartridge to build up substantial pressurewithin said expansion chamber prior to the rupturing of said burstdiaphragm, before accelerating the particulate load.
 6. The launchsystem according to claim 1, wherein said barrel includes quicklyremovable and reloadable barrels containing varying pre-packagedparticulate loads.
 7. The launch system according to claim 1, whereinsaid particulate loads contain a combination of one or more of powders,particulates, and projectiles.
 8. The launch system according to claim1, wherein said compressed gas cartridge contains compressed air.
 9. Thelaunch system according to claim 1, wherein said compressed gascartridge contains compressed nitrogen.
 10. The launch system accordingto claim 1, wherein said particulate load includes an irritant powder.11. The launch system according to claim 10, wherein said irritantpowder comprises a combination of inert powder and irritant powder toproduce an irritant cloud.
 12. The launch system according to claim 11,wherein said combination of inert and irritant powder further includes aheavy mass powder enabling said particulate load to travel effectivedistances from said launch system.
 13. The launch system according toclaim 12, wherein said heavy mass powder includes barium sulfate powder.14. The launch system according to claim 7, wherein said projectileincludes a projectile comprising a frangible membrane projectilecontaining a non-lethal combination mixture of irritant powder and heavymass powder.
 15. The launch system according to claim 14, wherein saidprojectile includes a projectile comprising a frangible membraneprojectile containing an inert heavy mass powder mixture alone fortraining purposes.
 16. A projectile for launching using a compressed gaslaunch system, comprising: a frangible plastic projectile containing anon-lethal, heavy mass irritant powder mixture; wherein said frangibleplastic projectile has sufficient mass to reach a distant target oncelaunched, and upon impact with the target produces an irritant cloudthat suspends in the air surrounding the target.
 17. The projectile forlaunching using a compressed gas launch system according to claim 16,wherein said non-lethal heavy mass irritant powder mixture includes acombination of one or more irritant powders and one or more heavy masspowders.
 18. The projectile for launching using a compressed gas launchsystem according to claim 16, wherein said heavy mass powders includebarium sulfate powder.
 19. The projectile for launching using acompressed gas launch system according to claim 16, wherein saidfrangible plastic projectile bursts upon impact with the target therebyallowing the irritant powder to form a visible cloud surrounding theimpacted target.
 20. The projectile for launching using a compressed gaslaunch system according to claim 19, wherein said irritant powder isreplaced with an inert powder for training purposes.